![Space technology / Wind tunnel / Drag / Hypersonic speed / Gas dynamics / Transonic speed / Mach number / Supersonic speed / USAF Digital DATCOM / Aerodynamics / Aerospace engineering / Aviation Space technology / Wind tunnel / Drag / Hypersonic speed / Gas dynamics / Transonic speed / Mach number / Supersonic speed / USAF Digital DATCOM / Aerodynamics / Aerospace engineering / Aviation](https://www.pdfsearch.io/img/9e1d317bafa2301f97ae3d07758d9ecb.jpg) Date: 2013-11-19 22:03:28Space technology Wind tunnel Drag Hypersonic speed Gas dynamics Transonic speed Mach number Supersonic speed USAF Digital DATCOM Aerodynamics Aerospace engineering Aviation | | 20th International Congress on Modelling and Simulation, Adelaide, Australia, 1–6 December 2013 www.mssanz.org.au/modsim2013 Comparison of computational and semi-empirical aerodynamics tools for making fit-for-purpose Add to Reading ListSource URL: www.mssanz.org.auDownload Document from Source Website File Size: 1,24 MBShare Document on Facebook
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